Elastomeric damper model and limit cycle oscillation in bearingless helicopter rotor blade

Citation metadata

Date: September-October 2000
From: Journal of Aircraft(Vol. 37, Issue 5)
Publisher: American Institute of Aeronautics and Astronautics Inc.
Document Type: Article
Length: 30 words

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Abstract :

Research is presented concerning the study of the transient response of the bearingless helicopter rotor blade in order to analyze the limit cycle. Two different models of elastomer were used.

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Source Citation   

Gale Document Number: GALE|A69274761